Saturn MS-II-4(S)B
Stage · USA
Original archive entry. The text, images and links below are kept as they were written.
LOx/LH2 propellant rocket stage. Standard S-II but with structural strength increased from 86% to 502% depending on station, resulting in 8.6% increase in empty weight.
No Engines: 5.
Related
- Country
- USA
- Engines
- J-2
- Launch Vehicles
- Saturn MLV-V-4(S), Saturn V-23(L), Saturn V-24(L), Saturn V-25(S)B, Saturn V-4X(U), Saturn V-25(S)U
- Propellants
- Lox/LH2